%0 Journal Article
%T Thermo-structural Analysis of Solid Rocket Scarfed Nozzle with Composite Ablative Liners for Crew Escape Solid Motor
%A Murugan, J. Paul
%A Kurian, Thomas
%A Levin, G.
%A Eswaran, V.
%A Jayaprakash, J.
%A Rajarajan, A.
%J "Advances in Astronautics Science and Technology"
%V 1
%N 1
%P 87-97
%@ 2524-5252
%D 2018-09-01
%I Springer Singapore
%~ DeepDyve